Engine Sump Air Separation via Windage-Suppressor Shroud

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Solution Overview

Problem

In gas turbine engines, the mixing of oil with high-pressure gases in the sump cavity disrupts the lubrication system, leading to inefficient lubricant distribution and potential oil loss through vent passageways, which complicates the management of air and oil flows.

Innovation Solution

An annular windage-suppressor shroud is designed to direct high-pressure gases from the seal gap into a vent passageway while preventing oil from mixing with these gases, using a guide passageway with radially-inwardly opening inlet and outlet, and guide vanes to ensure efficient air routing without oil entrainment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of substance

If high-pressure gases are allowed to mix with oil in the sump cavity, then the gases can be vented through the vent passageway, but oil is entrained and lost through the vents

Engineering Contradiction:
Improveoil lossVSAvoidair-oil separation complexity
Core Design Contradiction:
Loss of substanceVSDevice complexity

Solution Approach 1:

The sump cavity is segmented into distinct zones using a baffle structure that separates the gas flow path from the oil reservoir. The baffle creates a first region for gas venting and a second region for oil collection, preventing mixing while maintaining simple overall structure

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The high-pressure gases are extracted and directed through a dedicated guide passageway that bypasses the oil-containing region. The guide passageway with guide vanes channels gases directly to the vent passageway outlet, removing them from the sump cavity before they can entrain oil

Inventive Principle:
Principle #2Taking out (Extraction)

2Productivity

If the breather size is increased to handle air flow, then air handling capacity is improved, but the device size and weight increase

Engineering Contradiction:
Improveair handling efficiencyVSAvoidbreather weight
Core Design Contradiction:
ProductivityVSWeight of moving object

Solution Approach 1:

Guide vanes are introduced as intermediary elements within the guide passageway to actively direct and control the high-pressure gas flow. These vanes streamline the gas path, improving flow efficiency and reducing the required breather size while maintaining effective air handling capacity

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system changes the flow parameters by using guide vanes to optimize gas velocity and direction within the guide passageway. This controlled flow management allows for more efficient air handling with reduced component sizing

Inventive Principle:
Principle #35Parameter changes

3Productivity

If guide vanes are added to direct high-pressure gases, then air routing efficiency is improved, but device complexity increases

Engineering Contradiction:
Improvegas flow efficiencyVSAvoidshroud structure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The guide vanes are designed with specific geometric parameters including span, chord length, and twist distribution that optimize gas flow dynamics. The vanes create controlled flow patterns that efficiently direct high-pressure gases through the guide passageway while maintaining manageable structural complexity

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution effectively minimizes oil carried out through vents, allowing for efficient air handling and reduced breather size, maintaining oil distribution to bearings and reducing the risk of oil loss, thus optimizing the lubrication system's performance.

Implementation Method 1

The annular windage-suppressor shroud is located in the sump cavity and arranged circumferentially around the shaft assembly to direct the high-pressure gasses from the outlet of the seal gap to the vent passageway

Methodology Applied
Scientific EffectFluid flow direction control:

Implementation Method 2

The plurality of guide vanes may extend radially between the inner wall and the outer wall to direct the high-pressure gasses from the guide inlet toward the guide outlet

Methodology Applied
Scientific EffectFlow guidance:

Data Source

PatentEP3425161B1Engine sump with air separation features
Publication Date: 2020.03.18 ROLLS ROYCE CORP
  • EP3425161B1 patent drawingFigure 1~2
  • EP3425161B1 patent drawingFigure 3
  • EP3425161B1 patent drawingFigure 4

AI summary

A sump assembly for use in a gas turbine engine includes a housing and a shaft assembly. The housing is arranged about a central axis of the sump assembly to define a cavity configured to house oil and high-pressure gasses. The shaft assembly is mounted to rotate about the central axis and to direct the high-pressure gasses into the housing.